Single Engine • De Havilland • DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III, DHC-2-1000, Turbine-Beaver (PT6)
| Manufacturer | De Havilland |
| Model | DHC-2 Beaver |
| Category | Single Engine |
| Variants | DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III, DHC-2-1000, Turbine-Beaver (PT6) |
| Seating | 2, 6 seats |
| Typical TTAF | 6,500 hours |
| Markets | Canada, United States, Australia, New Zealand |
| Price Range | $180K – $850K |
The De Havilland DHC-2 Beaver is a legendary utility aircraft first introduced in 1947, renowned for its exceptional short-takeoff-and-landing (STOL) performance and rugged versatility. Designed in Canada, this high-wing, fabric-covered monoplane became an icon of bush flying and remote operations. The Beaver excels in delivering cargo and passengers to unprepared airstrips, gravel bars, water surfaces (on floats), and challenging terrain where conventional aircraft cannot operate. Its ability to carry substantial payload relative to its size, combined with dependable Pratt & Whitney engine reliability, made it indispensable for military operations, humanitarian missions, and commercial bush operators worldwide. The aircraft remains highly sought after in the used market, with many examples still actively flying after 70+ years. The Beaver's simple construction, ease of maintenance, and adaptability to various configurations—including amphibious floats and ski gear—have ensured its enduring appeal. It has served militaries, civilian operators, and adventure tourism companies across every continent, earning a reputation as one of aviation's most capable and dependable utility aircraft.
Maximum Speed: 160 mph (259 km/h)
Cruise Speed: 143 mph (230 km/h)
Range: 455 miles (732 km)
Service Ceiling: 18,000 feet (5,486 meters)
Engine: Pratt & Whitney R-985 Wasp Junior (450 hp)
Maximum Takeoff Weight: 5,090 lbs (2,310 kg)
Useful Load: 2,350 lbs (1,066 kg)
Takeoff Distance: 1,075 feet (328 meters, sea level)
Landing Distance: 735 feet (224 meters)